Shock-induced flow separation is the flow mechanism usually responsible for what the structural dynamicist terms 'buffet.' The shock-induced flow separation affects the aeroelastic response via two different mechanisms: (1) the flow separation generates fluctuating pressures, i.e., a forcing function that is independent of the motion of the aerodynamic surface, e.g., an aircraft wing, and (2) the flow separation affects the motion-dependent forces and can in some cases generate negative aerodynamic damping. A simple analysis is presented which, using static experimental data as an input, can predict these two buffet-components for a wing in high Mach number subsonic flow.
Dynamic effects of shock-induced flow separation.
Dynamics Specialists Conference ; 1973 ; Williamsburg, VA
01.03.1973
Aufsatz (Konferenz)
Keine Angabe
Englisch
Dynamic Effects of Shock-Induced Flow Separation
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